Numerical Simulations of the Performance of Scramjet Engine Model with Pylon Set Located in the Inlet
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Publisher
Springer Berlin Heidelberg
Link
http://link.springer.com/content/pdf/10.1007/978-3-642-17884-9_98.pdf
Reference10 articles.
1. Akyurtlu, A., Akyurtlu, J., Gonor, A.L., Khaikine, V., Cutler, A.D., Blankson, I.M.: Numerical and experimental tests of a supersonic inlet with Pylon Set and Fuel Injection through Pylons. AIAA 44th Aerospace Sciences Meeting, Reno, Nevada, USA. AIAA Paper 2006-1032 (2006)
2. Chernyi, G.G.: Gas Dynamics. CRC Press, New York, NY (1994)
3. Ferlemann, P.G.: Comparison of Hyper-X Mach 10 scramjet preflight prediction and flight data. AIAA/CIRA 13th International Space Planes and Hypersonic Systems and Technologies Conference, Capua, Italy. AIAA 2005-3352 (2005)
4. Ferlemann, S.M., McClinton, C.R., et al.: Hyper – X Mach 7 Scramjet design, ground test and fight results. AIAA/CIRA 13th International Space Planes and Hypersonic Systems and Technologies Conference, Capua, Italy. AIAA 2005-3322 (2005)
5. Gilinsky, M.M., Khaikine, V., Akyurtlu, A., Akyurtlu, J., Blankson, I.M., et al.: Numerical and experimental tests of a supersonic inlet utilizing a pylon set for mixing, combustion and thrust enhancement. AIAA/CIRA 13th International Space Planes and Hypersonic Systems and Technologies Conference, Capua, Italy. AIAA 2005-3290 (2005)
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